2 fatalities

2014-01-20: Britten-Norman Islander (YR-BNP) — Şcoala Superioară de Aviaţie Civilă — Petreasa, Romania

Petreasa, RomaniaFlight

On January 20, 2014, a Britten-Norman Islander (registration YR-BNP) operated by Şcoala Superioară de Aviaţie Civilă was involved in an aviation accident near Petreasa, Romania in flight. 2 people were killed. Investigators recorded the probable cause as: Double engine failure in flight due to carburetor icing. Contributing factors: erroneous assessment of risk factors, lack of crew experience, erroneous decisions by the captain regarding flight conditions, weight, and center of gravity. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781193785Data APIEditorial standards
Aircraft registered YR-BNP
Aircraft registered YR-BNP. Photo: Corneliu Bălan / CC BY-SA 3.0, via Wikimedia Commons

An ambulance flight from Bucharest to Oradea crashed in the Apuseni Mountains after both engines failed due to carburetor icing. One pilot and one passenger died, five others injured. The aircraft was destroyed.

Incident Details

The aircraft, a twin-engine aircraft, departed Bucharest-Baneasa Airport on an ambulance flight to Oradea. On board were two pilots, a medical team, and one patient. The purpose of the flight was to transport doctors to Oradea to obtain transplant organs from a deceased patient.

Sequence of Events

While cruising at an altitude of 6,300 feet over the Apuseni Mountain Range, the crew encountered marginal weather conditions with icing. Despite the conditions, the crew continued the flight. Subsequently, both engines lost power and failed. The crew attempted an emergency landing, but the aircraft collided with trees and crashed on a snowy, wooded hillside at an altitude of 1,400 metres.

Casualties and Damage

One pilot and one passenger were killed, while five other occupants were injured. The aircraft was destroyed.

Probable Cause

The official investigation determined the probable cause to be a double engine failure in flight due to carburetor icing. The following contributing factors were identified:

  • Erroneous assessment of the risk factors specific to the conduct of this flight.
  • Lack of crew experience on this type of aircraft.
  • Erroneous decision of the captain to continue the flight in meteorological conditions that caused the carburetor icing.
  • Erroneous decision of the captain to continue to fly for a long period of time in icing conditions.
  • Erroneous decision of the captain to continue the mission under the AMA, under conditions of BMI flight according to IFR flight rules.
  • Erroneous decision of the crew to initiate the flight while the total weight of the aircraft was above MTOW and the CofG was outside the prescribed limits.